Cal/avlabs Symposium Proceedings (3rd), 18-20 June 1969, Buffalo, New York. Aerodynamics of Rotary Wing and V/stol Aircraft. Volume Ii. Wind Tunnel Testing. New Concepts in Rotor Control PDF Download
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Author: CORNELL AERONAUTICAL LAB INC BUFFALO N Y.
Publisher:
ISBN:
Category :
Languages : en
Pages : 312
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Book Description
Contents: Model vs. full scale rotor testing; The flow throughout a wind tunnel containing a rotor with a sharply deflected wake; Comments on V/STOL wind tunnel data at low forward speeds; Problems associated with tunnel tests of high disk loading systems at low forward speeds; Some research on rotor circulation control; The aerodynamics of a circulation-controlled rotor; Higher harmonic pitch control; and The controllable twist rotor.
Author: CORNELL AERONAUTICAL LAB INC BUFFALO N Y.
Publisher:
ISBN:
Category :
Languages : en
Pages : 312
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Book Description
Contents: Model vs. full scale rotor testing; The flow throughout a wind tunnel containing a rotor with a sharply deflected wake; Comments on V/STOL wind tunnel data at low forward speeds; Problems associated with tunnel tests of high disk loading systems at low forward speeds; Some research on rotor circulation control; The aerodynamics of a circulation-controlled rotor; Higher harmonic pitch control; and The controllable twist rotor.
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Category : Rotors (Helicopters)
Languages : en
Pages : 174
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Author: Cornell University. Cornell Aeronautical Laboratory
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Category :
Languages : en
Pages :
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Author:
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Category : Rotors (Helicopters)
Languages : en
Pages : 186
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Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 100
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Author: CORNELL AERONAUTICAL LAB INC BUFFALO N Y.
Publisher:
ISBN:
Category :
Languages : en
Pages : 137
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Book Description
Contents: Welcome by host organizations; Keynote address; Now is the time for aerodynamics to come to the aid of the hardware; Recommendations for future aerodynamic research; Notes on rotor aerodynamic research; Suggestions toward a coordinated approach to aerodynamic research; Future aerodynamic research; Aerodynamic research related to propeller driven V/STOL aircraft; Panel discussion--question and answer period; and Some problems in the numerical solution of vortex motion equations.
Author:
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ISBN:
Category : Science
Languages : en
Pages : 260
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Author:
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ISBN:
Category : Science
Languages : en
Pages : 1340
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Category : Research
Languages : en
Pages : 1340
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Author:
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ISBN:
Category : Technology
Languages : en
Pages : 918
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